Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes
By: K.K. Ahuja and J. Mendoza.
Contributors: Mendoza, J.; Langley Research Center.
Series: NASA contractor report -- 4653.; NASA contractor report -- NASA CR-4653.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aeroacoustics.; Aerodynamic noise.; Cavities.; Cavity flow.; Subsonic flow.; Temperature effects.; Turbulent boundary layer.; Wall jets.; Wind tunnel tests.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0615-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 3 microfiches.